THEORETICAL AND EXPERIMENTAL INVESTIGATION OF THE SUBSONIC-FLOW FIELDS BENEATH SWEPT AND UNSWEPT WINGS WITH TABLES OF VORTEX-INDUCED VELOCITIES

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1956
Accession Number
AD0102814

Entities

People

  • William J. Alford Jr.

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Compressible Flow
  • Dynamic Pressure
  • Flow Fields
  • Free Stream
  • Incompressible Flow
  • Leading Edges
  • Load Distribution
  • Mach Number
  • Swept Wings
  • Sweptback Wings
  • Three Dimensional
  • Three Dimensional Flow
  • Two Dimensional Flow